Topology optimization with microstructures

ABSTRACT

System and method for optimizing a three-dimensional model representing a shape of an object to be fabricated from a plurality of materials having known physical properties. The object is designed to exhibit one or more target properties and the three-dimensional model includes a plurality of cells. The system includes at least one processor programmed to receive a data structure including information for a material property gamut of microstructures for the plurality of materials and two or more of the known physical properties of the plurality of materials, and perform a topology optimization process on the three-dimensional model to generate an optimized model, wherein the topology optimization process is constrained based, at least in part, on the information in the received data structure and the one or more target properties.

RELATE APPLICATIONS

The present application claims the benefit of U.S. Provisional PatentApplication No. 62/288,766, Jan. 29. 2016, titled “Topology Optimizationwith Microstructures,” which is hereby incorporated by reference in itsentirety.

STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT

This invention was made with Government support under Grant No.CCF-1533753 awarded by the National Science Foundation and Contract No.N66001-15-C-4030 awarded by the Space and Naval Warfare Systems Center.The Government has certain rights in the invention.”

BACKGROUND

Additive fabrication, e.g., 3-dimensional (3D) printing, providestechniques for fabricating objects, typically by causing portions of abuilding material to solidify and/or combine at specific locations.Additive fabrication techniques may include stereolithography, selectiveor fused deposition modeling, direct composite manufacturing, laminatedobject manufacturing, selective phase area deposition, multi-phase jetsolidification, ballistic particle manufacturing, particle deposition,laser sintering, polyjet, or combinations thereof. Many additivefabrication techniques build parts by forming successive layers, whichare typically cross-sections of the desired object. Typically each layeris formed such that it adheres to either a previously formed layer or asubstrate upon which the object is built.

SUMMARY

Some embodiments are directed to a system for optimizing athree-dimensional model representing a shape of an object to befabricated from a plurality of materials having known physicalproperties, wherein the object is designed to exhibit one or more targetproperties, wherein the three-dimensional model includes a plurality ofcells. The system comprises at least one processor configured to receivea data structure including information for a material property gamut ofmicrostructures for the plurality of materials and two or more of theknown physical properties of the plurality of materials and perform atopology optimization process on the three-dimensional model to generatean optimized model, wherein the topology optimization process isconstrained based, at least in part, on the information in the receiveddata structure and the one or more target properties.

Other embodiments are directed to a non-transitory computer-readablemedium comprising instructions that, when executed, perform a method ofoptimizing a three-dimensional model representing a shape of an objectto be fabricated from a plurality of materials having known physicalproperties, wherein the object is designed to exhibit one or more targetproperties, wherein the three-dimensional model includes a plurality ofcells. The method comprises receiving a data structure includinginformation for a material property gamut of microstructures for theplurality of materials and two or more of the known physical propertiesof the plurality of materials, and performing a topology optimizationprocess on the three-dimensional model to generate an optimized model,wherein the topology optimization process is constrained based, at leastin part, on the information in the received data structure and the oneor more target properties.

Other embodiments are directed to a method of optimizing athree-dimensional model representing a shape of an object to befabricated from a plurality of materials having known physicalproperties, wherein the object is designed to exhibit one or more targetproperties, wherein the three-dimensional model includes a plurality ofcells. The method comprises receiving a data structure includinginformation for a material property gamut of microstructures for theplurality of materials and two or more of the known physical propertiesof the plurality of materials, and performing a topology optimizationprocess on the three-dimensional model to generate an optimized model,wherein the topology optimization process is constrained based, at leastin part, on the information in the received data structure and the oneor more target properties.

The foregoing summary is provided by way of illustration and is notintended to be limiting.

BRIEF DESCRIPTION OF DRAWINGS

The accompanying drawings are not intended to be drawn to scale. In thedrawings, each identical or nearly identical component that isillustrated in various figures is represented by a like numeral. Forpurposes of clarity, not every component may be labeled in everydrawing. In the drawings:

FIG. 1 illustrates a process for optimizing a design of an object inaccordance with some embodiments;

FIG. 2 illustrates detailed steps of the process of FIG. 1 in accordancewith some embodiments;

FIGS. 3A-3C illustrate plots associated with a process for calculating amaterial property gamut in accordance with some embodiments;

FIG. 4 illustrates plots of level set gamuts that may be used ascontinuous material property gamuts in accordance with some embodiments;

FIG. 5 illustrates examples of material property gamuts calculated usingthe one or more of the techniques described herein in accordance withsome embodiments;

FIG. 6 illustrates plots of a simulation with a beam object inaccordance with some embodiments;

FIG. 7 illustrates plots of a simulation with a flexure mount object inaccordance with some embodiments;

FIG. 8 illustrates plots of a simulation with a gripper object inaccordance with some embodiments;

FIG. 9 illustrates a comparison between structures generated using aSIMP-based topology optimization process and a topology optimizationprocess performed in accordance with some embodiments;

FIG. 10 illustrates plots of a simulation with a bunny object inaccordance with some embodiments;

FIG. 11 illustrates plots of a simulation with a bridge object inaccordance with some embodiments; and

FIG. 12 illustrates an example of a computing system environment onwhich some embodiments may be implemented.

DETAILED DESCRIPTION

Some additive fabrication techniques allow an object to be fabricatedfrom more than one material. In order to instruct an additivefabrication device to fabricate an object from multiple materials, thetypes of materials may be specified for each part of the object prior tofabrication. For example, a designer of the object may use a softwareapplication to specify which regions of the object are to be fabricatedfrom which of the available materials. The object may then be fabricatedby depositing the specified material in each region during fabrication.

As the number of materials available for fabrication increases, however,the potential complexity in functional (e.g., mechanical, electrical,thermal, optical) characteristics of fabricated objects dramaticallyincreases. When provided with a desired set of functionalcharacteristics for a fabricated object, it can be both time consumingand, in some cases, difficult or impossible, for a user to specify whichmaterial should be deposited in each region of the object such that theobject can be fabricated with the desired functional characteristics.

For example, to design an object that compresses a particular way whensqueezed, a designer of the object may conventionally specify one ormore materials with which to fabricate the object, and where thosematerials should be located in the fabricated object, so that thefabricated object exhibits the desired compression characteristics. Thedesigner must consider the desired functional properties of a fabricatedobject and then decide how to put materials together so that incombination the materials make an object having those desired functionalproperties.

Some conventional approaches for determining a design of an objecthaving a particular shape and functional characteristics often usecomputational frameworks, an example of which is topology optimization.In topology optimization, an object is discretized into small volumeelements (voxels) and the material distribution over the voxels in theobjects is optimized in such a way that the object is fabricated withthe desired functional characteristics. For example, a material may beidentified for each voxel in the object, and by determining whichmaterial should be chosen for each voxel, a composition for the entireobject may be determined.

Recent multi-material 3D printing techniques provide the ability todesign objects with multiple materials at high resolution (e.g., 600 DPIor more), resulting in improved functional performance of the objects.Conventional topology optimization techniques generally do not scalewell and cannot practically be used to design objects with a largenumber (e.g., billions) of voxels since the number of variables tooptimize increases linearly with the number of voxels in the object. Forexample, for a 3D printer having a resolution of 600 DPI, a one billionvoxel design would occupy only a 1.67 inch cube. Designing largerobjects at or near the resolution of the printer would require designswith billions of voxels, further adding to the complexity of theoptimization problem. Some conventional techniques for dealing with thiscomplexity include using lower resolution designs with larger voxels andusing a non-uniform grid to model the object, resulting in a design withlower functional performance than desired.

The inventors have recognized and appreciated that conventional topologyoptimization techniques used with 3D printing applications may beimproved by modeling the object to be fabricated using microstructurescorresponding to groups of voxels rather than individual voxels.Previous attempts to use microstructures often decouple macro structuraldesign and micro material design by ignoring the geometry of themicrostructures and considering their macroscopic physical behaviorinstead. However, this approach introduces difficulties as the space ofmaterial properties covered by all possible printable microstructures ismuch wider than the properties of the base materials. For example,microstructures made of alternating layers of soft and stiff isotropicmaterials exhibit an anisotropic behavior as they are able to stretchmore easily in one direction than in the others. This implies that notonly the ranges but also the number of physical parameters needed todescribe the physical behavior of the microstructures increases.Accordingly, some embodiments are directed to techniques for addressing,at least in part, two challenging problems of working with the materialproperties of microstructures: (i) computing the gamut of the materialproperties achievable by all microstructures and (ii) optimizing thedistribution of the high-dimensional material properties inside thelayout of an object to be fabricated in an efficient way.

Some embodiments are directed to a novel computational framework fortopology optimization with microstructures that supports design spacesof multiple functional dimensions. The computational framework enablesefficient optimization of high resolution modes that can be fabricatedusing multi-material 3D printing. FIG. 1 illustrates a diagram of aprocess for a computational framework in accordance with someembodiments. In act 110, a gamut of material properties for a set ofmicrostructures is calculated. The material property gamut representsthe space of bulk material properties that can be achieved with allmaterial microstructures of a given size. In some embodiments, aprecomputation process is used that efficiently samples the space ofmicrostructures and their corresponding material properties to define amaterial property gamut. As discussed in more detail below, the gamutmay be computed by alternating stochastic sampling and continuousoptimization to provide a discrete representation of the materialproperties space from which a continuous representation of the gamut canbe constructed, for example, using a level set field.

The process of FIG. 1 then proceeds to act 120, where topologyoptimization constrained by the parameters of the continuous gamutrepresentation is performed to find optimal distributions of multiplematerial properties simultaneously inside the gamut. Using the gamut asa constraint in a generalized topology optimization framework enablesthe assignment of spatially varying material properties throughout theoptimized object.

The process of FIG. 1 then proceeds to act 130, where the output of thetopology optimization process is mapped onto the microstructures in thegamut computed in act 110 with corresponding properties to obtain a 3Dmodel for the object that can be fabricated using 3D printing. Each ofthe acts in the process of FIG. 1 is described in more detail below.

Some embodiments are directed to determining the material distributioninside an object that optimizes functional objectives given an objectlayout and a set of base materials. Microstructures made of the basematerials are used to compute a space or “gamut” of the physicalmaterial properties spanned by the microstructures. As used herein, theterm microstructure refers to a small scale assembly made of one or morebase materials that are used as low-level building blocks of an objectto be fabricated. The macroscale properties of the microstructure may bevery different from those of the original materials. Some aspects of thetechniques described herein are directed to combining a probabilisticsearch and a continuous optimization to explore the gamut of materialproperties that microstructures that can be achieved by assembling givenbase materials.

FIG. 2 shows a schematic diagram of a process for determining a materialdistribution inside an object in accordance with some embodiments. In afirst stage, the gamut of material properties covered by all possiblemicrostructures of a predefined size and made by spatial arrangement ofthe base materials is estimated. In a second stage, the precomputedmaterial property gamut is used to constrain a continuous topologyoptimization process to determine a physically realizable solutionmeeting desired functional characteristics. In a third stage, a 3Dprintable result is generated by replacing each voxel in the objectlayout with a microstructure having material properties closest to thecontinuous material assignment resulting from the optimization outputfrom the second stage.

Regarding the first stage, computing the mechanical properties ofmicrostructures, when arranged in periodic tilings, can be performed byprobing the structure using a physical simulation based on thehomogenization theory. While inferring the homogenized properties ofindividual microstructures is generally not computationally expensive,analyzing the space covered by all combinations of base materials ismuch more computationally complex due to the combinatorial explosion inthe number of possible material arrangements. For example, a lattice of16×16×16 voxels made up of only two materials corresponds to 2⁴⁰⁹⁶microstructures, and exhaustively probing all microstructures in thisspace is computationally infeasible. To address this issue, someembodiments (i) sample the space of the microstructures using discretesampling and (ii) rely on the continuity between material parameters ofthe individual voxels and macroscopic properties of the microstructuresin order to generate new microstructures with desired properties.

The inventors have recognized that although using continuousoptimization alone may be effective in reaching local optimal values inthe material property space, the function that maps the materialassignment to the material properties is nonlinear. In particular, verydifferent microstructures can correspond to the same point in thematerial property space. Additionally, since the ratio of materials ineach cell is bounded between zero and one, continuous optimizationconverges slowly or stops moving when material distributions in manyvoxels are at the lower or upper bound. Accordingly, being able to jumpout of a local optimum and discovering different variants provided bythe discrete sampling process is important to provide new explorationregions in the material property space. Accordingly, some embodimentsleverage a discrete sampling process 210 and a continuous optimizationprocess 212 by combining these techniques in a scheme that alternatesbetween a stochastic search and a continuous optimization, as shown inFIG. 2 and as discussed in more detail below.

Discrete Sampling

In accordance with some embodiments, discrete sampling process 210introduces discrete changes in the materials of the microstructures toallow for the emergence of new types of microstructures. Discretesampling may be achieved by sampling the space of material assignments,i.e., microstructures, in such a way that maximizes the number ofsamples corresponding to microstructures having material propertieslocated near the material property gamut boundaries. Rather than drawingall samples at once, a database of microstructures may be progressivelyenriched by refining the estimation of the material property gamutboundaries. The motivation behind this sampling strategy is theobservation that a small change in the material assignment of amicrostructure often translates to a small change of its materialproperties. By modifying microstructures located near the currentboundary of the gamut, it is likely that more microstructures will begenerated in this area of the gamut and some of those microstructureswill lie outside the boundaries of the current gamut, thereby expandingthe gamut when these microstructures are included in the database.

In some embodiments, a given microstructure is modified to generate newsamples by changing the material properties at random voxel locations inthe microstructure using a stochastically ordered sequential Monte Carlo(SOSMC) method. In the SOSMC method, a population of particlescorresponding to an instance of a procedural program are evolved so asto represent a desired distribution. During this process the programsare executed in a random order and particles are regularly scored andreallocated in regions of high probability. For example, the scoringfunction:

$\begin{matrix}{{s\left( p_{i} \right)} = {\frac{{dist}\left( p_{i} \right)}{\rho \left( p_{i} \right)} \times \frac{1}{\rho \left( p_{i} \right)}}} & (1)\end{matrix}$

may be used in some embodiments, where dist(p_(i)) measures the distanceof the properties of the microstructure corresponding to the particle ito the boundary of the gamut and ρ(p_(i)) is the local density ofmaterial points at the location p_(i). The material point density may bedefined as:

$\begin{matrix}{{\rho \left( p_{i} \right)} = {\sum\limits_{k}{\varphi_{k}\left( p_{i} \right)}}} & (2)\end{matrix}$

where

${\varphi_{k}(p)} = \left( {1 - \frac{{{p - p_{k}}}_{2}^{2}}{h^{2}}} \right)^{4}$

are locally-supported kernel functions that vanish beyond their supportradius h set to a tenth of the microstructure lattice size.

The first product in Eq. 1 favors microstructures located near theboundary of the gamut. The normalization by ρ allows to have the sameprobability to hit any location on the boundary. The second product inEq. 1 is used to additionally privilege under-sampled areas of thegamut.

In some embodiments, particles are resampled using a systematicresampling scheme that is also used to initiate the population ofparticles. The particles may then be evolved in accordance with thefollowing algorithm:

Example algorithm for generating new microstructures procedureGENMICROSTRUCTURE(input: microstructure M, output: microstructure m) m ←M while some voxels of m have not been visited do while microstructure mis unchanged do pick a random voxel v of m that has not been visited yetswap material of v with probability 0.5 if m is manifold and m ≠ M thenaccept the change end if end while end while end procedure

Continuous Optimization

Alternating with discrete sampling process 210 is a continuousoptimization process 212 that locally pushes the material space gamutboundaries by refining the microstructure shapes. In continuousoptimization process 212, the material distribution at each location inthe gamut is treated as a continuous variable enabling the formulationof continuous objective functions for exploring the material propertyspace. A subset of microstructures from the discrete samples determinedin the discrete sampling process 210 may be selected as starting pointsfor the continuous optimization.

For a given microstructure close to the boundary of the gamut, thedesired search direction may be determined using a level set field (orother suitable representation of the boundary of the gamut). The targetmaterial properties are then determined by moving the current propertiesalong the search direction. For example, material properties for cubicmicrostructures are described by the Young's modulus E, Poisson's ratioν, shear modulus μ, and average density ρ. These elasticity parametersmay be translated into six desired harmonic displacements and stackedinto a 6×6 matrix G₀. A goal of the continuous optimization process 212is to match the target coarse displacement G₀ and the target density bychanging the material distribution d at each cell. The objectivefunction may be written as:

ƒ(d)=(G(d)−G₀)² +w _(p)(ρ−ρ₀)   (3),

where w_(p) controls the weighting between the displacement term and thedensity term.

The derivative of the objective function may then be computed using theadjoint method as follows: Let K(d) be the stiffness matrix controlledby the material distribution d. For a given external force F_(ext), thedisplacements u of the fine degrees of freedom are u=K(d)⁻¹F_(ext). Letg(u) be a scalar function that depends on the displacements, then itspartial derivative with respect to the material distribution d′ at theith element is:

$\begin{matrix}{{u = {K^{- 1}F_{ext}}},} & (4) \\{{\lambda = {K^{- 1}\frac{\partial g}{\partial u}}},} & (5) \\{\frac{\partial g}{\partial d} = {\lambda \frac{\partial K_{i}}{\partial d_{i}}{u_{i}.}}} & (6)\end{matrix}$

The first two equations use the same matrix to solve for differentquantities and require only a single numerical factorization of thestiffness matrix K. Similarly, computing the derivatives of all 36entries in G needs only a single numerical factorization of thestiffness matrix K. With the gradient, a gradient descent may beperformed with a line search and bound constraints to find newmicrostructures. In some embodiments, a maximum number of gradient stepsis set at 500. After convergence or reaching a maximum number ofiterations, the material distributions may be thresholded to obtaindiscrete material assignments. Although the optimization operates in thecontinuous domain, the resulting microstructures generally exhibit adiscrete structure and have material properties that do not change muchafter thresholding.

Following continuous optimization of the microstructures in act 212, thediscrete sampling process 210 is repeated and cycling between discretesampling and continuous optimization continues until no significantexpansion of the gamut is observed or until some other criterion is met(e.g., a computational budget is reached). The output of the materialproperty gamut generation process is a discrete representation 214 ofthe material properties and the mapping between these properties and thecorresponding microstructures.

FIGS. 3A-3C shows plots of one cycle of computing a material propertygamut for the material properties Poisson's ratio and relative Young'smodulus, in accordance with some embodiments. Given a set of samples, asigned distance function is calculated as shown in FIG. 3A. The signeddistance function is used to find samples (e.g., samples p₁, p₂, p₃, p₄)located close to the boundary of the gamut, as shown in FIG. 3B. FIG. 3Balso shows that the gradient of the signed distance function providesnew search directions for each of the samples identified using thesigned distance function. A discrete search or a continuous optimizationbased on the identified samples may then be performed, as describedabove, to find new microstructures outside the current gamut therebyexpanding the gamut beyond its current boundaries, as shown in FIG. 3C.

Most available materials for 3D printers are elastic materials. Assumingsmall deformations, linear elasticity may be used to compute both themechanical behavior of the entire object and the microstructures. Insuch a setting, the relation between the linear strain ε and Cauchy'sstress σ at every material point is given by:

σ=εϵ,   (7)

where ε, the so-called elasticity tensor, can be described by 21parameters.

Working in such a high dimensional space is prohibitive and thereforematerials having a certain number of symmetries, such as orthotropicmaterials for which the elasticity tensor is defined by 12 parameters (4parameters for 2D), cubic materials defined by 3 parameters andisotropic materials defined by 2 parameters, are discussed herein foruse with some embodiments. For example, the tensor for a cubic structurecan be written (using the Voigt notation) as follows:

$\begin{matrix}{{\mathcal{E} = \begin{pmatrix}{\left( {1 - v} \right)\hat{E}} & {v\; \hat{E}} & {v\; \hat{E}} & \; & \; & \; \\{v\; \hat{E}} & {\left( {1 - v} \right)\hat{E}} & {v\; \hat{E}} & \; & \; & \; \\{v\; \hat{E}} & {v\; \hat{E}} & {\left( {1 - v} \right)\hat{E}} & \; & \; & \; \\\; & \; & \; & \mu & \; & \; \\\; & \; & \; & \; & \mu & \; \\\; & \; & \; & \; & \; & \mu\end{pmatrix}},} & (8)\end{matrix}$

where Ê=E|((1−2v)(1+v)), where E is the Young's modulus of the material,ν is its Poisson's ratio, and μ its shear modulus. Alternatively, Lame'sparameters can be used to define the tensor ε, which in this example hasthe form:

$\begin{matrix}{\mathcal{E} = {\begin{pmatrix}{{2\mu} + \lambda} & \lambda & \lambda & \; & \; & \; \\\lambda & {{2\mu} + \lambda} & \lambda & \; & \; & \; \\\lambda & \lambda & {{2\mu} + \lambda} & \; & \; & \; \\\; & \; & \; & \mu & \; & \; \\\; & \; & \; & \; & \mu & \; \\\; & \; & \; & \; & \; & \mu\end{pmatrix}.}} & (9)\end{matrix}$

Letting

=

″ denote the space of n material properties, each point p ϵ

may be written as [ρ, e], where ρ is the density of the material and eare the other material parameters.

Discretization

Using standard finite element techniques, an object may be discretizedinto regular voxels and its deformed state may be computed when subjectto external forces F_(ext) according to the relation:

Ku=F_(ext)   (10),

where K is the stiffness matrix of the system and u are thedisplacements at each of the nodes of the voxels. In some embodiments,this same approach is used to simulate both the mechanical behavior ofthe microstructures in the gamut representation 214 and the objectmacroscopic behavior, albeit at different scales. To simulate themicrostructures, each voxel may be assumed to be made of a homogeneousbase material, whereas for determining the large scale behavior of theobject, the object's cells may be assumed to correspond to amicrostructure whose properties are determined using numericalcoarsening. In some embodiments, the static equilibrium in Eq. 10 may besolved using a fast multigrid solver.

Continuous Material Property Gamut Representation

In accordance with some embodiments, the discrete gamut representationof microstructures 214 is transformed into a smooth continuous gamutrepresentation of the material property space to enable constrainedtopology optimization in the continuous material property space. In someembodiments, the continuous gamut representation is created using alevel set field that represents the boundary of the gamut. In otherembodiments, the continuous gamut representation may be created usingother suitable techniques for providing a smooth continuousrepresentation including, but not limited to, triangulation using amesh.

In some embodiments, the continuous representation of the materialproperty space is created by constructing a signed distance field fromthe point cloud in the precomputed material property space 214. Toconstruct the signed distance field when a level set field is used, thelevel set values may be stored on the cell centers of an n-dimensionalCartesian grid. Each component ϵ_(i) in the material property space maybe normalized by a linear interpolation function ε _(i)=N(ε_(i)) toconstrain the scope of the level set within an n-dimension unit cube.When a point on the level set is mapped to the material property space,the normalized value may be scaled back. Furthermore, the gradient ofthe interpolation function may also be considered when evaluating thematerial property gamut constraint using level set value interpolations.

In some embodiments, the signed distance field is generated from a setof points by assigning an implicit distance function φ(p) to each pointpϵ

. The signed distance field may be initialized using the implicitfunction φ(p)=∥p−p∥−r, where ∥□∥ is the Euclidean distance between twopoints in

and m is the average position of the neighboring points of p with adistance of r. The level set surface may then be smoothed by solving anexplicit mean curvature flow problem ∂φ/∂t=Δφ. For each time step, afast marching method may be run in a dimension n to reinitialize thesigned distance values over the entire domain.

FIG. 4 shows examples of level set gamuts that may be generated and/orused in accordance with some embodiments. The representations in the toprow of FIG. 4 (from left to right) show the 3-dimensional level sets fora 2D isotropic material space parameterized by the density ρ, thenormalized Young's modulus E and the Poisson's ratio ν.; for a 3Disotropic material space parameterized by ρ, Ê and v; for a 2D isotropicmaterial space parameterized by the density ρ and the Lamé's parameters;and for a 3D isotropic material space parameterized by the density ρ andthe Lamé's parameters. The representations in the middle row of FIG. 4(from left to right) show a projection of the sample points in the (ρ,Ê, σ) material space; and three slices of the 4-dimensional level setsfor cubic 2D, microstructures in the (ρ, Ê, σ) material space. Therepresentations in the bottom row of FIG. 4 (from left to right) show aprojection of the sample points in the (ρ, Ê, σ) material space; andthree slices of the 4-dimensional level sets for cubic 3Dmicrostructures in the (ρ, Ê, σ) material space.

In accordance with some embodiments, a topology optimization problem isreformulated directly in the continuous representation of the materialproperty gamut to enable a continuous constrained topology optimizationprocess 220. Such an approach minimizes the objective function overpossible material parameters while requiring strict satisfaction of thephysics constraints (e.g., static equilibrium) as well as strictsatisfaction of the physical parameter bounds. When a level set field isused to create the continuous representation of the material propertygamut, the physical parameter bounds constraint can be formulated aslimiting the material properties to stay on the negative side of thelevel set to ensure that the material properties used in theoptimization are physically realizable.

Topology Optimization

Some conventional topology optimization problems optimize the shape andstructure of a given object defined by a prescribed domain in order tominimize a cost function. For example, the compliance of an object maybe minimized while satisfying static equilibrium and total weightconstraints. Since the topology of the object is unknown a priori, theshape of the object may be defined through its material distribution andthe material densities may be worked with locally. To this end, thethree-dimensional model of the design layout may be converted into cells(e.g., 10×10×10 voxel cubes) and a density variable may be assigned toevery cell of the discretized layout.

Some embodiments extend conventional topology optimization processes inat least two ways. First, computation of a binary material distributionis not needed, as the database of microstructures represented in theprecomputed material property gamut are used to fill each cell of theoptimized solution. Leveraging the continuous representation of thematerial property gamut, each cell is only required to have materialproperties inside the gamut. Second, the constrained topologyoptimization process in accordance with some embodiments can be usedwith more complex parameterizations of the material property space thanconventional topology optimization processes, which are usuallyformulated with a single unknown density for each cell. The continuousconstrained topology optimization process 220 in accordance with someembodiments is schematically illustrated in FIG. 2, which shows thatboth the domain and external conditions related to the object (e.g., adiscretized version of the object to be fabricated) and thepre-calculated material property gamut 214 provide constraints on thetopology optimization process.

In some embodiments, each cell c_(i) contains an n-dimensional materialparameter p_(i)ϵ

, where p is used to denote the stacked vector of material parameters inall cells. Given a signed distance function Φ(p_(i)) that defines thegamut, a topology optimization problem in accordance with someembodiments is given as follows:

$\begin{matrix}{{{{{\min\limits_{p}{\text{:}\mspace{14mu} {\left( {p,u} \right)}}}s.t.\text{:}}\mspace{14mu} \left( {p,u} \right)} = {0:{{\Phi \left( p_{i} \right)} \leq 0}}},{1 \leq i \leq N_{i}},} & (11)\end{matrix}$

where

is a real-valued objective function that depends on the materialparameters and the displacement vector u of the entire object at theelasticity equilibrium. The equality constraint

=0 requires u to satisfy the elasticity equilibrium and the inequalityconstraint Φ≤0 guarantees that the material properties of each cellstays inside the boundaries of the precomputed gamut.

In the examples described herein, the material parameter p consists ofthe density ρ and the elasticity parameters e. However, it should beappreciated that any suitable number and combination of materialproperties may be used as the material parameter p, and embodiments arenot limited in this respect. In some embodiments that include density ρand the elasticity parameters e as material parameter p, the objectivefunction may be split into a density term σ(ρ) that controls the overallmass and an elasticity term

(e,u) that controls the deformation behavior. These terms can beweighted for specific topology optimization problems. The density termcan be written as:

$\begin{matrix}{{{v(\rho)} = \left( {{\sum\limits_{i = 1}^{N}{\rho_{i}V_{i}}} - \hat{M}} \right)^{2}},} & (12)\end{matrix}$

where V_(i) is the cell volume and {circumflex over (M)} is the targetoverall weight. Alternatively, the total weight objective may be treatedas an equality constraint. In some embodiments, density is not treatedas a special variable. In practice, a very large coefficient canpreserve the target overall weight very well, if needed. For particulartopology optimization problems, spatially varying weight control termsmay be added to the density term above. For example, the target weightof each individual cell may be controlled by adding a logical term(ρ_(s)−{circumflex over (ρ)}_(s))²V_(i).

The elasticity constraint may be written as

(e,u)=K(e)u−f=0. The gamut constraint for a point in the materialproperty space may be described by an n-dimensional level set functionΦ(p), where Φ(p)<0 for a point inside the gamut, Φ(p)>0 for a pointoutside the gamut, and Φ(p)=0 for a point on the boundary of the gamut.The value of Φ represents the m-dimension Euclidean distance to thelevel set boundary. In some embodiments, this distance is linearlyinterpolated from the precomputed signed distance field. The gradient ofΦ can be evaluated by a finite difference operation on the signeddistance field.

In some embodiments, two types of objective functions may be used forthe elasticity term in the topology optimization process 220. The firsttype of objective function is target deformation, which relates tocontrolling the deformation of an object by designing its internalstructures. In some embodiments, a vector of the nodal targetdisplacements and the boundary conditions are taken as input to thetopology optimization process. Then the optimal material distributionover the object domain is automatically generated to achieve the desireddeformation within the range of linear elastic behavior. The deformationobjective may be defined as:

(e, u)=(u−û)^(T) D(u−û)   (13),

where û is a vector of target displacements and D is a diagonal matrixthat determines the importance of each nodal displacement. D may be usedto define the subset of nodes of interest. For example, most entries ofD may be set to zero to focus on a portion of the domain. The weightscan also be defined based on cell densities by setting D_(i,j)=ρ_(k)^(k) where k is a power index controlling the effect of the cell densityon the target deformation.

The second type of objective function is minimum compliance. In minimumcompliance, the deformation objective

is defined as the negative elastic potential energy:

(e, u)=u ^(T) K(e)u   (14).

In some conventional topology optimization problems, the elementstiffness matrix K_(i) depends on the artificial density value x,through an analytical formula such as K_(i)=x_(i) ³K_(D). In contrast,the stiffness matrix in the minimum compliance objective function inaccordance with some embodiments depends only on elasticity parameterssuch as the Young's modulus and the Poisson's ratio, and the constraintposed by density is enforced through the precomputed material propertygamut.

Microstructure Substitution

As discussed above, a 3D printable design may be generated by replacingeach cell in the optimized object layout with a microstructure from thematerial property gamut whose material properties are closest to thecontinuous material assignment resulting from the topology optimizationprocess. This microstructure substitution process 230 results in acomplex, high-resolution multi-material model with optimized functionalspecifications that may be used as input to a 3D printing process. Insome situations, multiple microstructures in the material property gamutmay have the same material properties, and one of the multiplemicrostructures may be selected during microstructure substitutionprocess 230. The microstructure selected for substitution may beselected using any suitable criterion including, but not limited to, ameasure of continuity between the microstructure and the microstructuresin adjacent cells of the design layout. Additionally, in someembodiments, one or more post-processing steps may be used to provide aprintable solution that improves the continuity between adjacent cellsof the design layout.

Validation

The microstructure sampling techniques described herein were analyzedfor 2D and 3D microstructure gamuts made of one or two materials. Forthe 2D case, patterns with cubic and orthotropic mechanical behaviorsthat can be described with four parameters (three elasticity parametersand density) and five parameters (four elasticity parameters anddensity), respectively, were considered. In 3D, the gamut correspondingto cubic structures with four parameters was computed. In all cases, thesize of the lattice for the microstructures was set to 16 voxels inevery dimension. Isotropic based materials whose Young's modulusdiffered by a factor of 100 and having 0.48 as Poisson's ratio wereused. For microstructures made of a single material, the softer materialwas used for the empty cells, and all disconnected components generatedduring the sampling stage were removed.

The resulting gamuts are shown in FIG. 5. The gamut on the left of FIG.5 was computed for 2D cubic structures and contained 274 kmicrostructures, the gamut in the middle of FIG. 5 was computed for 2Dorthotropic structures and contained 388 k microstructures, and thegamut on the right of FIG. 5 was computed for 3D cubic structures andcontained 88 k microstructures. Generation of these gamuts took from 15hours to 93 hours to compute, which correspond to 68, 19 and 5 samplingcycles, respectively. The plots show the results for the projection ofthe gamuts on the plane defined by the macroscale Young's modulus alongthe x-axis (normalized by the Young's modulus of the stiffest basematerial) and the Poisson's ratio corresponding to a contraction alongthe y-direction when the material is stretched along the x-direction.

A significant increase in the coverage of the material space wasobserved compared to a conventional approach for generating a materialproperty gamut, even for 2D microstructures where a coarserdiscretization was used. These results confirm that topologyoptimization only, while helpful to locally improve the microstructuregeometries, is suboptimal when attempting to discover the entire gamutof physical properties. The diversity of microstructures obtained wasalso much richer than the conventional approach for generating amaterial property gamut, thereby providing a large set of options forthe practical use of microstructures. Additionally, even when nosampling of the interior space of the gamut was explicitly enforced,these areas showed a dense sampling as a result of the randomness of thesampling technique, reducing the need to run costly optimization inthese areas.

The continuous constrained topology optimization processes in accordancewith some embodiments, were also used to compute a wide variety ofmodels in different settings. The sizes and computation times of theresulting models are outlined in Table 1 below.

TABLE 1 List of optimized models with microstructures. Time per Time perGrid # Material FEM Solve step Example Size Voxels Space [s] [s]Deformation Beam 96 × 24 × 4  38M cubic/iso .7 5 Flexure 32 × 32 × 1667M iso 1 12 Gripper 64 × 32 × 8  67M cubic/iso 1.7 10 Compliance Bunny32 × 32 × 32 134M  cubic .6 4 Bridge 128 × 64 × 32  1074M  iso 27 81

Since a line search is performed at each gradient step, it may takemultiple simulations to take one step. The average time required fortaking a step is shown in the last column of Table 1. On average, ittook two hundred iterations to find a local minimum, though it may bepossible to improve the speed further by using different optimizationroutines.

Small-scale tests were used to validate the topology optimizationtechniques described herein. Beams were computed to match differenttarget poses. FIG. 6 shows four optimized beams with differentdeformation targets. The top two beams achieve their target states undersqueezing and the bottom row of beams uses stretching. The beam wassqueezed or stretched by setting Dirichlet boundary conditions on itstwo sides. The optimization was run on an isotropic Lame space and thetarget volume was selected to be 0.2.

A first set of examples was designed using the target deformationobjective. FIG. 7 shows the design and optimization of a flexure mountstructure with two deformation targets. The design goal of the structurewas to design a flexure that resists vertical loads while remainingcomplaint in the horizontal direction. The top of the flexure was fixedto be a circular shape so that other parts could be mounted as shown inthe top left portion of FIG. 7. Two sets of external forces were appliedto the circle. Under a vertical load, the flexure should stay close tothe rest shape while under horizontal load the flexure should deformaccording to the top right portion of FIG. 7. The bottom left and rightportions of FIG. 7 show two fabricated flexure designs with differenttarget overall weights.

FIG. 8 illustrates designs of different gripper structures generatedusing the topology optimization techniques described herein. The designgoal was to achieve the grasping deformation of the head of the gripperwhen a user pressed the two ends. Use of the topology optimizationtechnique in accordance with some embodiments enabled the automaticdesign of complex 3D structures composed of a variety of microstructuresthat can achieve the target deformation. By changing the parameter ofthe desired volume, different designs relying on either in-planedeformation (left column of FIG. 8) or out-of-plane bending (rightcolumn of FIG. 8) that can both achieve the same target motion wereproduced.

The efficacy and scalability of the topology optimization techniquedescribed herein on solving the minimum compliance problem wasdemonstrated by designing and fabricating different objects. Thetechnique was validated on classic topology optimization problems suchas cantilever beam and bridge. When the topology optimization techniquewas restricted to using only the density and Young's modulus asoptimization variables, the technique was able to find the same solutionas a conventional solid isotropic material with penalisation(SIMP)-based topology optimization technique. This was expected sinceconventional techniques use the boundary of an artificialstiffness-density curve controlled by the power index. When thePoisson's ratio was added as an optimization variable, the minimumcompliance objective function reached 10% lower energy than theconventional technique. As the parameter space was increased to includecubic materials, the advantage over the conventional technique wasincreased to 15% as shown in FIG. 9. The left plot in FIG. 9 showsstructures generated with a conventional SIMP-based topologyoptimization technique and the right plot in FIG. 9 shows structuresgenerated using the topology optimization technique described herein.

To demonstrate the scalability of the topology optimization techniquedescribed herein, the technique was used on a Stanford bunny to minimizethe object's compliance under two different external loads, as shown inFIG. 10. The two sets of external forces were applied to the back andchest of the bunny as shown in the top left portion of FIG. 10. Materialparameters were computed and color coded where lighter colors indicatelarger parameter values as shown in the top right portion of FIG. 10.The nearest microstructures were substituted as shown in the bottom leftof FIG. 10 to create the optimized design, and the model shown in thebottom right of FIG. 10 was fabricated.

FIG. 11 shows the design of a bridge structure within a rectangularvolume using the topology optimization technique described herein. Agrid with 500 k cells, which corresponds to one billion voxels aftersubstitution of the microstructures for each cell was used. As shown inthe upper left portion of FIG. 11, the initial volume was a 128×64×32regular grid. A uniform downward loading force was applied and thematerial parameters were computed and the cells with extremely lowstiffness were set to be void material as shown in the top right portionof FIG. 11. Appropriate microstructures were substituted as shown in thelower left portion of FIG. 11 and the bridge structure shown in thelower right portion of FIG. 11 was 3D printed.

Although discussed in the context of 3D printing applications, thetopology optimization techniques described herein can be applied to alarge variety of optimization problems and embodiments are not limitedin this respect.

FIG. 12 illustrates an example of a suitable computing systemenvironment 1200 on which aspects of the invention may be implemented.For example, the computing system environment 1200 may be used todetermine the supportedness of one or more regions of an object, togenerate a support structure for an object, to generate support tips fora support structure, to indicate the supportedness of one or moreregions of an object via a graphical user interface, to interface withone or more devices to effect additive fabrication of an object and/or asupport structure, or any combinations thereof. Such a computingenvironment may represent a home computer, a tablet, a mobile device, aserver and/or any another computing device.

The computing system environment 1200 is only one example of a suitablecomputing environment and is not intended to suggest any limitation asto the scope of use or functionality of the invention. Neither shouldthe computing environment 1200 be interpreted as having any dependencyor requirement relating to any one or combination of componentsillustrated in the exemplary operating environment 1200.

Aspects of the invention are operational with numerous other generalpurpose or special purpose computing system environments orconfigurations. Examples of well-known computing systems, environments,and/or configurations that may be suitable for use with the inventioninclude, but are not limited to, personal computers, server computers,hand-held or laptop devices, multiprocessor systems,microprocessor-based systems, set top boxes, programmable consumerelectronics, network PCs, minicomputers, mainframe computers,distributed computing environments that include any of the above systemsor devices, and the like.

The computing environment may execute computer-executable instructions,such as program modules. Generally, program modules include routines,programs, objects, components, data structures, etc. that performparticular tasks or implement particular abstract data types. Theinvention may also be practiced in distributed computing environmentswhere tasks are performed by remote processing devices that are linkedthrough a communications network. In a distributed computingenvironment, program modules may be located in both local and remotecomputer storage media including memory storage devices.

With reference to FIG. 12 an exemplary system for implementing aspectsof the invention includes a general purpose computing device in the formof a computer 1210. Components of computer 1210 may include, but are notlimited to, a processing unit 1220, a system memory 1230, and a systembus 1221 that couples various system components including the systemmemory to the processing unit 1220. The system bus 1221 may be any ofseveral types of bus structures including a memory bus or memorycontroller, a peripheral bus, and a local bus using any of a variety ofbus architectures. By way of example, and not limitation, sucharchitectures include Industry Standard Architecture (ISA) bus, MicroChannel Architecture (MCA) bus, Enhanced ISA (EISA) bus, VideoElectronics Standards Association (VESA) local bus, and PeripheralComponent Interconnect (PCI) bus also known as Mezzanine bus.

Computer 1210 typically includes a variety of non-transitory computerreadable media. Computer readable media can be any available media thatcan be accessed by computer 1210 and includes both volatile andnonvolatile media, removable and non-removable media. By way of example,and not limitation, computer readable media may comprise computerstorage media and communication media. Computer storage media includesboth volatile and nonvolatile, removable and non-removable mediaimplemented in any method or technology for storage of information suchas computer readable instructions, data structures, program modules orother data. Computer storage media includes, but is not limited to, RAM,ROM, EEPROM, flash memory or other memory technology, CD-ROM, digitalversatile disks (DVD) or other optical disk storage, magnetic cassettes,magnetic tape, magnetic disk storage or other magnetic storage devices,or any other medium which can be used to store the desired informationand which can accessed by computer 1210. Communication media typicallyembodies computer readable instructions, data structures, programmodules or other data in a modulated data signal such as a carrier waveor other transport mechanism and includes any information deliverymedia. The term “modulated data signal” means a signal that has one ormore of its characteristics set or changed in such a manner as to encodeinformation in the signal. By way of example, and not limitation,communication media includes wired media such as a wired network ordirect-wired connection, and wireless media such as acoustic, RF,infrared and other wireless media. Combinations of the any of the aboveshould also be included within the scope of computer readable media.

The system memory 1230 includes computer storage media in the form ofvolatile and/or nonvolatile memory such as read only memory (ROM) 1231and random access memory (RAM) 1232. A basic input/output system 1233(BIOS), containing the basic routines that help to transfer informationbetween elements within computer 1210, such as during start-up, istypically stored in ROM 1231. RAM 1232 typically contains data and/orprogram modules that are immediately accessible to and/or presentlybeing operated on by processing unit 1220. By way of example, and notlimitation, FIG. 12 illustrates operating system 1234, applicationprograms 1235, other program modules 1236, and program data 1237.

The computer 1210 may also include other removable/non-removable,volatile/nonvolatile computer storage media. By way of example only,FIG. 12 illustrates a hard disk drive 1241 that reads from or writes tonon-removable, nonvolatile magnetic media, a magnetic disk drive 1251that reads from or writes to a removable, nonvolatile magnetic disk1252, and an optical disk drive 1255 that reads from or writes to aremovable, nonvolatile optical disk 1256 such as a CD ROM or otheroptical media. Other removable/non-removable, volatile/nonvolatilecomputer storage media that can be used in the exemplary operatingenvironment include, but are not limited to, magnetic tape cassettes,flash memory cards, digital versatile disks, digital video tape, solidstate RAM, solid state ROM, and the like. The hard disk drive 1241 istypically connected to the system bus 1221 through an non-removablememory interface such as interface 1240, and magnetic disk drive 1251and optical disk drive 1255 are typically connected to the system bus1221 by a removable memory interface, such as interface 1250.

The drives and their associated computer storage media discussed aboveand illustrated in FIG. 12, provide storage of computer readableinstructions, data structures, program modules and other data for thecomputer 1210. In FIG. 12, for example, hard disk drive 1241 isillustrated as storing operating system 1244, application programs 1245,other program modules 1246, and program data 1247. Note that thesecomponents can either be the same as or different from operating system1234, application programs 1235, other program modules 1236, and programdata 1237. Operating system 1244, application programs 1245, otherprogram modules 1246, and program data 1247 are given different numbershere to illustrate that, at a minimum, they are different copies. A usermay enter commands and information into the computer 1210 through inputdevices such as a keyboard 1262 and pointing device 1261, commonlyreferred to as a mouse, trackball or touch pad. Other input devices (notshown) may include a microphone, joystick, game pad, satellite dish,scanner, or the like. These and other input devices are often connectedto the processing unit 1220 through a user input interface 1260 that iscoupled to the system bus, but may be connected by other interface andbus structures, such as a parallel port, game port or a universal serialbus (USB). A monitor 1291 or other type of display device is alsoconnected to the system bus 1221 via an interface, such as a videointerface 1290. In addition to the monitor, computers may also includeother peripheral output devices such as speakers 1297 and printer 1296,which may be connected through a output peripheral interface 1295.

The computer 1210 may operate in a networked environment using logicalconnections to one or more remote computers, such as a remote computer1280. The remote computer 1280 may be a personal computer, a server, arouter, a network PC, a peer device or other common network node, andtypically includes many or all of the elements described above relativeto the computer 1210, although only a memory storage device 1281 hasbeen illustrated in FIG. 12. The logical connections depicted in FIG. 12include a local area network (LAN) 1271 and a wide area network (WAN)1273, but may also include other networks. Such networking environmentsare commonplace in offices, enterprise-wide computer networks, intranetsand the Internet.

When used in a LAN networking environment, the computer 1210 isconnected to the LAN 1271 through a network interface or adapter 1270.When used in a WAN networking environment, the computer 1210 typicallyincludes a modem 1272 or other means for establishing communicationsover the WAN 1273, such as the Internet. The modem 1272, which may beinternal or external, may be connected to the system bus 1221 via theuser input interface 1260, or other appropriate mechanism. In anetworked environment, program modules depicted relative to the computer1210, or portions thereof, may be stored in the remote memory storagedevice. By way of example, and not limitation, FIG. 12 illustratesremote application programs 1285 as residing on memory device 1281. Itwill be appreciated that the network connections shown are exemplary andother means of establishing a communications link between the computersmay be used.

The various methods or processes outlined herein may be implemented inany suitable hardware. Additionally, the various methods or processesoutlined herein may be implemented in a combination of hardware and ofsoftware executable on one or more processors that employ any one of avariety of operating systems or platforms. Any suitable combination ofhardware and software may be employed to realize any of the embodimentsdiscussed herein.

In this respect, various inventive concepts may be embodied as at leastone non-transitory computer readable storage medium (e.g., a computermemory, one or more floppy discs, compact discs, optical discs, magnetictapes, flash memories, circuit configurations in Field Programmable GateArrays or other semiconductor devices, etc.) encoded with one or moreprograms that, when executed on one or more computers or otherprocessors, implement the various embodiments of the present invention.The non-transitory computer-readable medium or media may betransportable, such that the program or programs stored thereon may beloaded onto any computer resource to implement various aspects of thepresent invention as discussed above.

The terms “program” or “software” are used herein in a generic sense torefer to any type of computer code or set of computer-executableinstructions that can be employed to program a computer or otherprocessor to implement various aspects of embodiments as discussedabove. Additionally, it should be appreciated that according to oneaspect, one or more computer programs that when executed perform methodsof the present invention need not reside on a single computer orprocessor, but may be distributed in a modular fashion among differentcomputers or processors to implement various aspects of the presentinvention.

Computer-executable instructions may be in many forms, such as programmodules, executed by one or more computers or other devices. Generally,program modules include routines, programs, objects, components, datastructures, etc. that perform particular tasks or implement particularabstract data types. Typically, the functionality of the program modulesmay be combined or distributed as desired in various embodiments.

Having herein described several embodiments, several advantages ofembodiments of the present application should be apparent. One advantageis that an object may be designed based on any number of availablematerials such that the object, when fabricated, exhibits one or moredesired properties. A non-limiting list of applications for whichembodiments described herein may be used include optics, mechanicalengineering, industrial design, aerospace design, musical instruments,toys and games, and combinations thereof.

Furthermore, the techniques described herein may, in some embodiments,provide in an approach to designing an object that is modular,extensible, independent of object geometry and/or independent of afabrication device which may be used to subsequently fabricate theobject. In some embodiments, a design of an object may be determinedindependently of a type of fabrication device that may be subsequentlyused to fabricate the designed object. For example, while one or morematerial properties may be provided as input to the design process,these materials may not uniquely correspond to a particular fabricationdevice or fabrication process.

Various inputs to the design of a three-dimensional object have beendiscussed above, and it will be appreciated that any number of inputsmay be considered in designing an object using the techniques describedherein. A non-limiting list of suitable inputs may include an inputshape (e.g., a geometrical object), one or more desired properties ofthe object to be designed, a simulation configuration (e.g., the numberand type of simulations, the parameters describing a composition of theobject that are associated with each simulation, etc.), one or morematerials from which the object may be fabricated, one or moreproperties of the one or more materials (e.g., mechanical properties,cost, weight/density, thermal properties, electrical properties, etc.),details on a fabrication technique (e.g., specifications of an additivefabrication system, such as a resolution; time to fabrication based onan object composition), or combinations thereof.

An input shape may be described using any suitable format, including anydata that defines a three-dimensional geometry (e.g., by definingpositions of vertices, normals and/or faces). A non-limiting list ofsuitable formats for an input shape may include STereoLithography (STL),Wavefront OBJ, Additive Manufacturing File Format (AMF), ObjDF,Stratasys SLC, Zmodeler Z3D, Lightwave LWO, Autodesk Maya and/or 3DStudio Max, etc.

While techniques described herein have, in some cases, been described asdesigning an object suitable for use in additive fabrication, it will beappreciated that the techniques described herein are not limited todesigning objects to be fabricated using additive fabrication, and maybe used to design an object completely independent of whether anysubsequent fabrication of the object might occur. For example, thetechniques described herein may be used to design an object that is notfabricated, which may be useful, for example, for a designer to explorehow an object might be designed without taking the step of physicallyfabricating the object. In use cases in which an object designed usingone or more of the techniques described herein is fabricated, anysuitable type of fabrication approach may be used including, but notlimited to, additive fabrication (including stereolithography, selectiveor fused deposition modeling, direct composite manufacturing, laminatedobject manufacturing, selective phase area deposition, multi-phase jetsolidification, ballistic particle manufacturing, particle deposition,laser sintering, polyjet, or combinations thereof), computer numericalcontrol (CNC) machining, or any combination thereof.

Various inventive concepts may be embodied as one or more methods, ofwhich examples have been provided. The acts performed as part of anymethod described herein may be ordered in any suitable way. Accordingly,embodiments may be constructed in which acts are performed in an orderdifferent than illustrated, which may include performing some actssimultaneously, even though shown as sequential acts in illustrativeembodiments.

All definitions, as defined and used herein, should be understood tocontrol over dictionary definitions, definitions in documentsincorporated by reference, and/or ordinary meanings of the definedterms.

The indefinite articles “a” and “an,” as used herein, unless clearlyindicated to the contrary, should be understood to mean “at least one.”

As used herein, the phrase “at least one,” in reference to a list of oneor more elements, should be understood to mean at least one elementselected from any one or more of the elements in the list of elements,but not necessarily including at least one of each and every elementspecifically listed within the list of elements and not excluding anycombinations of elements in the list of elements. This definition alsoallows that elements may optionally be present other than the elementsspecifically identified within the list of elements to which the phrase“at least one” refers, whether related or unrelated to those elementsspecifically identified.

The phrase “and/or,” as used herein, should be understood to mean“either or both” of the elements so conjoined, i.e., elements that areconjunctively present in some cases and disjunctively present in othercases. Multiple elements listed with “and/or” should be construed in thesame fashion, i.e., “one or more” of the elements so conjoined. Otherelements may optionally be present other than the elements specificallyidentified by the “and/or” clause, whether related or unrelated to thoseelements specifically identified. Thus, as a non-limiting example, areference to “A and/or B”, when used in conjunction with open-endedlanguage such as “comprising” can refer, in one embodiment, to A only(optionally including elements other than B); in another embodiment, toB only (optionally including elements other than A); in yet anotherembodiment, to both A and B (optionally including other elements); etc.

As used herein, “or” should be understood to have the same meaning as“and/or” as defined above. For example, when separating items in a list,“or” or “and/or” shall be interpreted as being inclusive, i.e., theinclusion of at least one, but also including more than one, of a numberor list of elements, and, optionally, additional unlisted items. Onlyterms clearly indicated to the contrary, such as “only one of” or“exactly one of,” will refer to the inclusion of exactly one element ofa number or list of elements. In general, the term “or” as used hereinshall only be interpreted as indicating exclusive alternatives (i.e.“one or the other but not both”) when preceded by terms of exclusivity,such as “either,” “one of,” “only one of,” or “exactly one of.”

The phraseology and terminology used herein is for the purpose ofdescription and should not be regarded as limiting. The use of“including,” “comprising,” “having,” “containing”, “involving”, andvariations thereof, is meant to encompass the items listed thereafterand additional items.

Having described several embodiments of the invention in detail, variousmodifications and improvements will readily occur to those skilled inthe art. Such modifications and improvements are intended to be withinthe spirit and scope of the invention. Accordingly, the foregoingdescription is by way of example only, and is not intended as limiting.

What is claimed is:
 1. A system for optimizing a three-dimensional modelrepresenting a shape of an object to be fabricated from a plurality ofmaterials having known physical properties, wherein the object isdesigned to exhibit one or more target properties, wherein thethree-dimensional model includes a plurality of cells, the systemcomprising: at least one processor configured to: receive a datastructure including information for a material property gamut ofmicrostructures for the plurality of materials and two or more of theknown physical properties of the plurality of materials; and perform atopology optimization process on the three-dimensional model to generatean optimized model, wherein the topology optimization process isconstrained based, at least in part, on the information in the receiveddata structure and the one or more target properties.
 2. The system ofclaim 1, wherein the at least one processor is further programmed to:generate a printable design for the object by substituting for each cellof the optimized model, a microstructure from the material propertygamut of microstructures, wherein the substituted microstructure hasphysical properties similar to material properties assigned to the cellby the topology optimization process.
 3. The system of claim 2, whereinthe data structure includes a mapping between each of themicrostructures in the material property gamut and the two or morephysical properties of the plurality of materials, and whereinsubstituting a microstructure from the material property gamut ofmicrostructures comprises substituting the microstructure based on themapping.
 4. The system of claim 1, wherein the precomputed materialproperty gamut of microstructures is a continuous representation of thematerial property gamut, and wherein performing a topology optimizationprocess comprises: formulating a continuous objective function; andoptimizing the continuous objective function constrained by the materialproperties represented in the continuous representation of the materialproperty gamut.
 5. The system of claim 4, wherein the continuousrepresentation of the material property gamut is a level setrepresentation.
 6. The system of claim 1, wherein the at least oneprocessor is further programmed to: performing a computation process tocompute the information for the material property gamut ofmicrostructures by estimating a gamut of material properties covered byall possible microstructures made by spatial arrangement of theplurality of materials; and wherein receiving the data structureincluding the information for the material property gamut ofmicrostructures comprises receiving the output of the computationprocess.
 7. The system of claim 6, wherein computing the information forthe material property gamut of microstructures comprises alternating adiscrete sampling process and a continuous optimization process toexpand the boundary of the material property gamut.
 8. The system ofclaim 6, wherein the output of the computation process is a discreterepresentation of the material property gamut, and wherein the at leastone processor is further programmed to: generate a continuousrepresentation of the material property gamut; wherein performing atopology optimization process comprises performing the topologyoptimization process based, at least in part, on the continuousrepresentation of the material property gamut.
 9. A non-transitorycomputer-readable medium comprising instructions that, when executed,perform a method of optimizing a three-dimensional model representing ashape of an object to be fabricated from a plurality of materials havingknown physical properties, wherein the object is designed to exhibit oneor more target properties, wherein the three-dimensional model includesa plurality of cells, the method comprising: receiving a data structureincluding information for a material property gamut of microstructuresfor the plurality of materials and two or more of the known physicalproperties of the plurality of materials; and performing a topologyoptimization process on the three-dimensional model to generate anoptimized model, wherein the topology optimization process isconstrained based, at least in part, on the information in the receiveddata structure and the one or more target properties.
 10. Thenon-transitory computer-readable medium of claim 9, wherein the methodfurther comprises: generating a printable design for the object bysubstituting for each cell of the optimized model, a microstructure fromthe material property gamut of microstructures, wherein the substitutedmicrostructure has physical properties similar to material propertiesassigned to the cell by the topology optimization process.
 11. Thenon-transitory computer-readable medium of claim 10, wherein the datastructure includes a mapping between each of the microstructures in thematerial property gamut and the two or more physical properties of theplurality of materials, and wherein substituting a microstructure fromthe material property gamut of microstructures comprises substitutingthe microstructure based on the mapping.
 12. The non-transitorycomputer-readable medium of claim 9, wherein the precomputed materialproperty gamut of microstructures is a continuous representation of thematerial property gamut, and wherein performing a topology optimizationprocess comprises: formulating a continuous objective function; andoptimizing the continuous objective function constrained by the materialproperties represented in the continuous representation of the materialproperty gamut.
 13. The non-transitory computer-readable medium of claim12, wherein the continuous representation of the material property gamutis a level set representation.
 14. The non-transitory computer-readablemedium of claim 9, wherein the method further comprises: performing acomputation process to compute the information for the material propertygamut of microstructures by estimating a gamut of material propertiescovered by all possible microstructures made by spatial arrangement ofthe plurality of materials; and wherein receiving the data structureincluding the information for the material property gamut ofmicrostructures comprises receiving the output of the computationprocess.
 15. The non-transitory computer-readable medium of claim 14,wherein computing the information for the material property gamut ofmicrostructures comprises alternating a discrete sampling process and acontinuous optimization process to expand the boundary of the materialproperty gamut.
 16. The non-transitory computer-readable medium of claim14, wherein the output of the computation process is a discreterepresentation of the material property gamut, and wherein the methodfurther comprises: generating a continuous representation of thematerial property gamut; wherein performing a topology optimizationprocess comprises performing the topology optimization process based, atleast in part, on the continuous representation of the material propertygamut.
 17. A method of optimizing a three-dimensional model representinga shape of an object to be fabricated from a plurality of materialshaving known physical properties, wherein the object is designed toexhibit one or more target properties, wherein the three-dimensionalmodel includes a plurality of cells, the method comprising: receiving adata structure including information for a material property gamut ofmicrostructures for the plurality of materials and two or more of theknown physical properties of the plurality of materials; and performinga topology optimization process on the three-dimensional model togenerate an optimized model, wherein the topology optimization processis constrained based, at least in part, on the information in thereceived data structure and the one or more target properties.
 18. Themethod of claim 17, further comprising: generating a printable designfor the object by substituting for each cell of the optimized model, amicrostructure from the material property gamut of microstructures,wherein the substituted microstructure has physical properties similarto material properties assigned to the cell by the topology optimizationprocess.
 19. The method of claim 17, wherein the precomputed materialproperty gamut of microstructures is a continuous representation of thematerial property gamut, and wherein performing a topology optimizationprocess comprises: formulating a continuous objective function; andoptimizing the continuous objective function constrained by the materialproperties represented in the continuous representation of the materialproperty gamut.
 20. The method of claim 19, wherein the continuousrepresentation of the material property gamut is a level setrepresentation.